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Airworthiness Directives

NOTE - This AD note listing is intended as a guide only and should not be relied upon as conclusive evidence of AD applicability on any particular aircraft. Entire Airworthiness Directives may be accessed at:

Showing Results 421 - 440 of 5103 | View All
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AD No. MAKE Condensed description of ad note
09-8-11 Pilatus Install an overboard vent for the airfoil deice system pressure regulator | PC12 and PC12/45
09-8-10 Pilatus Superseded by 10-5-2
09-8-1 Honeywell Supersedes 07-7-12 | Inspect NZ-2000 nav computer for affected serial numbers and comply as specified | Various aircraft
09-7-8 Piper Insert "operate only under day VFR rules" into the AFM until inspection of the 35-amp and 250-amp current limiters are done as specified | Pa-46-350P and 46R-350T
09-7-52 Bell Helicopter Supersedes 09-7-51 | Inspect the cyclic control lever assembly and determine if affected bearing SN is installed correctly as specified on assemblies less then 50 hours TIS | 206A,-B,-L, 407, 427
09-7-51 Bell Helicopter Superseded by 09-7-52
09-7-2 Hawker Beechcraft Supersedes 96-3-7 | Install adjustment mechanism on crew seats; replace aluminum assemblies | 400,-A; MU-300-10
09-7-14 Diamond Inspect the adhesive joint between the wing main spar caps and the upper wing skin for adhesive voids as specified | DA40
09-6-5 Bombardier This AD is in regards to cracking of the wing anti-ice piccolo ducts and their inspection/prevention as specified | CL-600,-601,-6013A,-6013R,-604
09-6-1 Eurocopter Determine the orientation of the fixed connector "24 Delta" and if the large contacts are not oriented "aft," re-orient the fixed connector so that they are facing "aft" as specified | EC 155B, B1
09-5-9 Bell Helicopter Superseded by 13-20-51
09-5-7 Pilatus Supersedes 08-6-17 | Inspect the stick-pusher servo-cables for correct installation, position, and tension as specified | PC12/45, /47, /47E
09-5-5 Avidyne Inspect PFD for affected serial numbers listed in the AD and do the required actions as specified | Multiple aircraft
09-5-12 Cessna Modify the aileron carry-through cable attachment to the aileron upper quadrant with parts of improved design as specified | 208 & 208B
09-4-9 DeHavilland Supersedes 08-11-10 | Install inspection holes in the left and right lower wing skins and inspect front spar adapter assemblies for cracks as specified | DHC-6-200, -300
09-4-4 Cessna Using Cessna SB MEB08-8, inspect the auxiliary wing spar near the location where the main landing gear trunnion is mounted for cracks as specified | 401/A/B, 402/A/B
09-4-3 Rolls-Royce AD issued to prevent low-cycle fatigue of the parts listed, see AD | AE 3007A1E and AE 1107C
09-4-14 Pilatus Superseded by 09-8-10
09-3-5 Pratt & Whitney Inspect the CT disc bore area for damage and replace as specified | PW206A - E, PW207C - E
09-3-4 Turbomeca Superseded by 12-23-12

Showing Results 421 - 440 of 5103 | View All
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